| 高载荷质量比复合材料机翼模型结构设计与制造研究 |
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| 引用本文： | 胡江波,梁宪珠,张铖,陈向明,杨宇. 高载荷质量比复合材料机翼模型结构设计与制造研究[J]. 材料开发与应用, 2011, 26(3): 37-40 |
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| 作者姓名： | 胡江波 梁宪珠 张铖 陈向明 杨宇 |
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| 作者单位： | 北京航空制造工程研究所;中国飞机强度研究所; |
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| 摘 要： | 针对给定外形机翼模型,为得到具有高载荷质量比的模型机翼,提出3种结构布局形式,结合有限元计算结果与制造工艺性分析,最终确定直梁式机翼结构布局方案.提出的成形工艺方案,通过成形质量检验和加载试验,验证了成形工艺的可行性和合理性.
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| 关 键 词： | 高载荷质量比 机翼模型 成形工艺 预浸料填充物 |
Study on Structure Design and Manufacture of High Load-weight Ratio Composite Wing Model |
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| HU Jiang-bo,LIANG Xian-zhu,ZHANG Cheng,CHEN Xiang-ming,YANG Yu. Study on Structure Design and Manufacture of High Load-weight Ratio Composite Wing Model[J]. Development and Application of Materials, 2011, 26(3): 37-40 |
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| Authors: | HU Jiang-bo LIANG Xian-zhu ZHANG Cheng CHEN Xiang-ming YANG Yu |
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| Affiliation: | HU Jiang-bo1,LIANG Xian-zhu1,ZHANG Cheng1,CHEN Xiang-ming2,YANG Yu2(1.Beijing Aeronautical Manufacturing Technology Research Institute,Beijing 100024,China,2.Aircraft Strength Research Institute of China,Xi'an 710065,China) |
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| Abstract: | In accordance with the outline of the wing model given and in order to achieve high load-weight ratio of the wing,three layouts of wing structure are presented.One of them,the straight-beam layout,is determined after analysis of simulation of FEM and manufacture process.The forming process has been advanced,which is proved feasible and reasonable through the forming-quality verification and load test. |
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| Keywords: | High load-weight ratio Wing model Forming process Prepreg filler |
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